The Study of the Asymmetric Multiple Encounters Problem and Its Application to Obtain Jupiter Gravity Assisted Maneuvers

Table 2

Swing-by with Δ𝑉>1.2, Δ𝑉, and Δ𝐸 in canonical units.

𝑒 = 0.1
𝜓𝑜 = −2.5 rad		Angle of approach		Variation of velocity	Variation of energy
𝜓𝑠 = 3.5 rad
𝜓𝑓		𝜓𝐴		Δ𝑉	Δ𝐸
rad	Degree	rad	Degree
2.999	171.830043	3.8745	221.992498	1.2159	0.81346
3.001	171.944634	3.8770	222.135737	1.2144	0.81472
−1.001	−57.3530753	3.8902	222.892041	1.2053	0.82042
1.999	114.534263	3.8795	222.278977	1.2119	0.81532
2.001	114.648855	3.8801	222.313354	1.2116	0.81562
2.999	171.830043	3.8607	221.201816	1.2222	0.80505
3.001	171.944634	3.8607	221.201816	1.2222	0.80509
1.999	114.534263	3.8882	222.77745	1.2113	0.82266
2.001	114.648855	3.8871	222.714425	1.2119	0.82209
2.999	171.830043	3.8857	222.63421	1.2125	0.82121
1.999	114.534263	3.8900	222.880582	1.2067	0.82113
2.999	171.830043	3.8857	222.63421	1.2125	0.82121
3.001	171.944634	3.8817	222.405027	1.2146	0.81913
1.999	114.534263	3.8900	222.880582	1.2067	0.82113
1.999	114.534263	3.8882	222.77745	1.2113	0.82266
2.001	114.648855	3.8871	222.714425	1.2119	0.82209
2.999	171.830043	3.8607	221.201816	1.2222	0.80505
3.001	171.944634	3.8607	221.201816	1.2222	0.80509